Blade damper

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing

Reexamination Certificate

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Details

C416S500000

Reexamination Certificate

active

06932575

ABSTRACT:
A turbomachine blade damper has a damper member with first and second damping surfaces for respectively engaging first and second surfaces of adjacent first and second blades. The damper has a seal having a first portion engaged in the damper member to resist relative movement of the seal in at least one direction and a second portion engaging at least one of the blades and advantageously forming a seal to resist upstream gas infiltration.

REFERENCES:
patent: 4872810 (1989-10-01), Brown et al.
patent: 4872812 (1989-10-01), Hendley
patent: 5226784 (1993-07-01), Mueller et al.
patent: 5228835 (1993-07-01), Chlus
patent: 5302085 (1994-04-01), Dietz et al.
patent: 5369882 (1994-12-01), Dietz et al.
patent: 5478207 (1995-12-01), Stec
patent: 5513955 (1996-05-01), Barcza
patent: 5827047 (1998-10-01), Gonsor et al.
patent: 1167691 (2002-01-01), None
patent: 402095702 (1990-04-01), None

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